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CFM56-7B26E/B1 ✕ V2527-A5 ✕
Family CFM56-7B
EASA ID 01P11CM117 1IA003
Aircraft Engine Manufacturer CFM International International Aero Engines
Aircraft Engine Type Turbofan Turbofan
Comment Boeing 737 Next Generation
Dry Weight (kg) 2366
Diameter (mm) 1549
Max Rotating Diameter (mm) 1549
Length (mm) 2507
Wikipedia Article (URL) en.wikipedia.org/wiki/CFM_International_CFM56
Fuel Jet A Jet A
Fan Blades 24
Geared Fan No No
Low-Pressure Compressor Stages 3
High-Pressure Compressor Stages 9
Combustion Chamber Tech Insertion
High Pressure Compressor Stages 1
Low-Pressure Turbine Stages 4
Afterburner No No
Streams 2 2
Bypass Ratio 5.1 4.82
Overall Pressure Ratio 27.7 27.2
Maximum Takeoff Thrust (kN) 117 111.2
Hydrocarbon Take Off (g/kg fuel) 0.02 0.041
Hydrocarbon Climb Out (g/kg fuel) 0.02 0.041
Hydrocarbon Approach (g/kg fuel) 0.05 0.061
Hydrocarbon Idle (g/kg fuel) 1.75 0.105
Hydrocarbon Unitary Average (g/kN) 2.58 0.29
Hydrocarbon Unitary Sigma (g/kN) 0.37
Hydrocarbon Unitary Range (g/kN) 2.18-2.91
Hydrocarbon Unitary Characteristic (g/kN) 3.01 0.4
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 15.4 2.3
Hydrocarbon LTO (g) 302 32
Carbon Monoxide Take Off (g/kg fuel) 0.2 0.53
Carbon Monoxide Climb Out (g/kg fuel) 0.16 0.62
Carbon Monoxide Approach (g/kg fuel) 3.07 2.44
Carbon Monoxide Idle (g/kg fuel) 30.94 12.43
Carbon Monoxide Unitary Average (g/kN) 46.81 24.9
Carbon Monoxide Unitary SD (g/kN) 2.6
Carbon Monoxide Unitary Range (g/kN) 43.8-48.7
Carbon Monoxide Unitary Characteristic (g/kN) 50.6 30.6
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 42.9 25.9
NOx Take Off (g/kg fuel) 21.79 26.5
NOx Climb Out (g/kg fuel) 17.08 22.3
NOx Approach (g/kg fuel) 8.93 8.9
NOx Idle (g/kg fuel) 4.27 4.7
NOx Unitary Average (g/kN) 40.71 48.5
NOx Unitary SD (g/kN) 1.2
NOx Unitary Range (g/kN) 39.8-42.1
NOx Unitary Characteristic (g/kN) 43.1 56.2
NOx Unitaryto Standard (% of limit) 45.2 59.6
NOx Unitaryto CAEP2 (% of limit) 56.5 74.4
NOx Unitaryto CAEP4 (% of limit) 68.1 89.9
NOx Unitaryto CAEP6 (% of limit) 77.3 102.2
NOx Unitaryto CAEP8 (% of limit) 91.9 121.7
NOx LTO (g) 4762 5382
Smoke Take Off (SN) 13.1 5.2
Smoke Climb Out (SN) 9.8 7.2
Smoke Approach (SN) 2.1 4.2
Smoke Idle (SN) 2.1 2.6
Smoke Max (SN) 13.07 9
Smoke Sigma (SN) 4.1
Smoke Range (SN) 8.4-16.2
Smoke Characteristic (SN) 14.37 11.6
Smoke Characteristicto Regulatory (% of limit) 63.4 50.4
Fuel Flow Take Off (kg/s) 1.213 1.053
Fuel Flow Climbout (kg/s) 0.986 0.88
Fuel Flow Approach (kg/s) 0.331 0.319
Fuel Flow Idle (kg/s) 0.108 0.128
Fuel LTO (kg) 429 437
Fuel Venting Compliant Yes No
Carbon Monoxide LTO (g) 5476 2764
Compressor Description 1 fan, 3-stage LP, 9-stage HP
Emissions Data Status C C
Engine Status Out of production Out of production
NOx Compliance Demonstration 2.3.2 e)
nvPME Imass Approach (mg/kg) 1.57
nvPME Imass Climb Out (mg/kg) 40.3
nvPME Imass Idle (mg/kg) 0.75
nvPME Imass Max (mg/kg) 61.8
nvPME Imass Take Off (mg/kg) 61.8
nvPME Inum Approach (#/kg) 65400000000000
nvPME Inum Climb Out (#/kg) 433000000000000
nvPME Inum Idle (#/kg) 29500000000000
nvPME Inum Max (#/kg) 433000000000000
nvPME Inum Take Off (#/kg) 415000000000000
nvPMLTO Mass (mg) 8646
nvPMLTO Mass Per Thrust (mg/kN) 103
nvPMLTO Mass To CAEP11 (% of limit) 23.3
nvPMLTO Number (#) 87700000000000000
nvPMLTO Number Per Thrust (#/kN) 1040000000000000
nvPMLTO Number To CAEP11 (% of limit) 19.3
nvPM Mass Concentration Characteristic (mg/m³) 1936
nvPM Mass Concentration Max (mg/m³) 1504
nvPM Mass Concentration To CAEP10 (% of limit) 31.6
Turbine Description 1-stage HP, 4-stage LP